COMPUTATION OF THE HEAT CYCLES OF INTERNAL COMBUSTION TURBINES BY A COMPUTER (VYPOCET TEPELNYCH OBEHU SPALOVACICH TURBIN NA SAMOCINNEM POCITACI),
Abstract
By the example of a three-shaft gas turbine the advantages are demonstrated of using computers for a more accurate calculation of gas cycles. While conventional methods of calculation disregard or simplify many factors, computers can include them in their programs. In the example, the following quantities are included in the formulas: thermodynamic losses in turbines and compressors expressed in isoentropy efficiency, pressure losses, thermal and mechanical losses, losses of the working medium, and combustion process efficiency. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 15, 1967
- Accession Number
- AD0841524
Entities
People
- B. Kurz
Organizations
- National Air and Space Intelligence Center